simulative analysis and experimental investigation of
TRANSCRIPT
The 13th Scandinavian International Conference on Fluid Power, SICFP2013, June 3-5, 2013, Linköping, Sweden
Simulative Analysis and experimental Investigation of Common Rail Injection
Pumps lubricated with tailor-made Biofuels
S. Heitzig, S. Drumm and H. Murrenhoff
Institute for Fluid Power Drives and Controls (IFAS), RWTH Aachen University, Aachen, Germany
E-mail: [email protected],
Abstract
In the scope of the cluster of excellence “Tailor-Made Fuels from Biomass” new biofuels are
developed within an interdisciplinary research approach at RWTH Aachen University. The most
promising fuel candidates so far tend to have a low viscosity and a low lubricity compared to
diesel fuel. It is the task of the authors to develop a guideline for designing injection systems
that are especially adapted to these fuels. The main focus is on high pressure pump within
common rail systems. In this paper, the effects of those fuel candidates on the tribological
contacts in standard common rail pumps are investigated by means of experiments and
simulations. On the experimental side a test rig is presented, which allows the measurement of
the transversal force on a piston and the friction force, which occur in the piston/bushing-
contact. On the simulation side, elastohydrodynamic simulation models of several tribological
contacts within the standard pump are presented. Results of simulation and measurement are
presented.
Keywords: Elastohydrodynamic simulation, friction forces, tribological contacts, common rail
pump, fuels, journal bearings
1 Introduction and Motivation
1.1 Tailor-made Fuels from Biomass
Environmental pollution and the exploitation of non-
renewable resources of modern times force the development
of new sustainable biofuels. One approach to find such
biofuels is pursued within the cluster of excellence “Tailor-
Made Fuels from Biomass” at RWTH Aachen University.
Within the cluster, new biofuels are developed and tested in
an interdisciplinary approach, see fig. 1.
Figure 1: Tailor-made Fuels from Biomass
The fluids are evaluated regarding their suitability for use as
a biofuel on the basis of their conversion, combustion and
tribological characteristic. A lot of the investigated fuels
have an excellent combustion and canversion characteristic
but poor tribological properties. They can differ severely
from conventional fuels in their lubrication and viscosity
characteristics. Therefore, tribological problems and higher
efforts to pressurise the fuel to the injection pressure level
have to be expected in fuel-lubricated common rail pumps
when operated with the new fuel candidates. In order to
facilitate a widespread usage of potential new biofuels,
research at the Institute for Fluid Power Drives and
Controls (IFAS) focuses on two approaches to ensure a
proper functioning of the tribological systems. On the one
hand, low-lubricity biofuels can be blended with high-
lubricity biofuels in order to enhance their lubrication
characteristics in the boundary lubrication regime [1, 2]. On
the other hand, research on the components reveals what
extent modifications of those components (micro and macro
geometry, materials, coatings, etc.) can contribute reducing
the effort that is necessary in order to pressurise the fuel
candidates.
1.2 Common Rail Injection Pump
Diesel injection systems of modern passenger cars are
nowadays generally designed as so-called common rail
systems. In those systems the pressure build-up is decoupled
from the injection process by means of the so-called rail,
which functions as a hydraulic accumulator. In this paper
the focus is on the common rail pump, which is used to
pressurise the fuel to the injection pressure level. From the
437
hydraulic point of view this is a challenging task for several
reasons. Firstly, the pressure level of common rail systems is
much higher than in standard hydraulic applications.
Systems of the first generation started with a maximum
pressure level of 1350 bar. In the second and third
generation the maximum pressure level was increased in
order to achieve a more efficient combustion and fewer
emissions. To fulfill the upcoming regulation regarding
future emission limits, the next generation of common rail
systems will operate at even higher pressures from 2500 up
to 3000 bar. Secondly, from a tribological point of view the
fluid properties of diesel are worse in comparison to
standard hydraulic fluid. According to DIN EN 590, at
40 °C diesel has a viscosity within the range from 2,0 up to
4,5 mm2/s. This leads to more leakage losses in pumps and
more operation of the tribological contacts in the mixed and
boundary lubrication regime. And thirdly, those pumps are
for the rather cost sensitive automotive sector.
Figure 2: Common rail pump CP1. Source: Robert Bosch
GmbH
As a starting point the effects of the fuel candidates on a
standard common rail pump of the first generation are
studied in this paper. This kind of pump, a BOSCH CP1 [3],
is a radial piston type design and consist of three pistons, see
fig. 2. Via a metal sheet clamp, each piston is connected to a
piston slipper, which is sliding on a planar surface of the
polygon ring. This ring is connected via a rotational journal
bearing to the eccentric shoulder of the pump drive shaft.
All tribological contacts in this pump are lubricated by the
fuel itself.
Figure 3: Sequence of one revolution
In fig. 3 the kinematics of this kind of pump are illustrated
for the movement of one piston unit. The revolution starts at
0° drive shaft angel with the transition from the compression
stroke to the suction stroke. The piston is at the outer dead
center (ODC) and hence its velocity is zero. From 0° to 180°
the suction stroke is continuous and the piston moves
downwards. At 90° the direction of the relative motion in
the sliding contact between slipper and polygon changes its
direction. At 180° the piston is at the inner dead center
(IDC) of its movement. From 180° to 360° the compression
stroke is continuous and the piston moves upwards again.
At closer inspection of cross section of the pump in fig. 2 it
becomes obvious that there is a slight displacement d
between the axis of each piston and the axis of the drive
shaft. This detail in design, which can be found in every
common rail pump of this type, is exemplified in fig. 4.
Figure 4: Tilting of the polygon ring
The motivation for this displacement d is a reduction of the
tilting φ of the polygon ring. This tilting is determined by
the forces acting on the polygon ring. In the investigated
pump type each piston axis has a displacement d to the drive
axis of half the eccentricity e of the drive shaft. With this
displacement the tilting of the polygon ring is reduced and
hence the transversal load Fx on each piston, see eq. 1.
costan FFFFFzxxx
(1)
If no tilting occurs (φ = 0), the transversal load Fx is equal to
the friction force Fµ in the polygon/slipper-contact, because
the bearing surface on the polygon is orthogonal to the axis
of the piston. As soon as the polygon is tilted (φ ≠ 0), a
transversal force Fxφ due to the inclined plane has to be
taken into account.
1.3 Focus of this Paper
Within the scope of this paper simulative and experimental
approaches investigating the effects of the new fuel
candidates on standard common rail pumps are discussed.
The presented experimental approach tries to cover the
operating characteristic and conditions of standard pumps as
realistic as possible. But nevertheless, a few differences
occur between the operating characteristic and conditions in
the test rig and in a standard pump. This experimental
approach allows the measurement of the friction force in the
piston/bushing-contact as well as the transversal load on the
piston. In the simulative approach further contacts are taken
into consideration to reach a better comparability of
measurement and simulation. As this paper will
demonstrate, there are several specific reasons why a
satisfying comparability of measurement and simulation is
piston
drive shaft
slipper
polygon
bushing
SSsS suction stroke
SSsS compression stroke
S
S
s
S
0°/360° 90° 180° 270°
ODC
IDC
438
difficult to reach at this point. Improvements on the
experimental side will be exposed, which will enable a
better comparability in the future.
2 Experimental Approach
2.1 Test Rig Set-Up
Over the past decades several test rigs were designed to
measure the friction forces in tribological contacts within
hydraulic pumps [4] [5] [6] [7] [8]. The basic principle
chosen for this test rig is comparable to the one developed
by Breuer [9].
The design of the test rig is shown in fig. 5 (a). This design
allows the measurement of the friction force (z-direction)
and the transversal load (x-direction) of one piston unit. All
tribologically relevant parts are taken from standard pumps
(piston, bushing, piston slipper, polygon ring, drive shaft).
One bushing is separated from the housing and connected to
the force measurement platform. In order to compensate the
huge forces occurring because of the pressure build-up in
the piston chamber, a compensation piston with the same
diameter is installed. This piston transmits the pressure
forces directly to the base frame so that these forces are not
measured by the force sensors.
Figure 5: Test rig, layout (a) and hydraulic diagram (b)
Figure 5 (b) shows the hydraulic diagram of the rig. A
simple external gear pump is used as a fuel feeding pump.
To achieve a constant supply pressure of 6 bar a pressure
relieve valve is installed. Two check valves at each piston
are used for commutation. The flow of the pistons is
pumped to two different common rails (accumulators). One
rail is connected to the measured piston while the other rail
is supplied by the unmodified pistons. The pressure in each
common rail is controlled by a pressure relieve valve. By
means of the use of two common rails it is achieved that
only low pressure connections are installed between the
platform measuring the force and the base frame of the test
rig. That is how no additional forces develope because of
pressure pulsation in the high pressure system are induced to
the force measuring system.
A more detailed description of the test rig can be seen in
[10].
2.2 Comparison of Test Rig and Standard Pump
Even though operating conditions of the tribological
contacts in the test rig are similar to those in standard
pumps, there are a few differences. In the following, these
differences will be discussed.
In order to separate the pressure forces from the friction
forces a compensation piston is added to the test rig. This
will slow down the pressure build-up in the piston chamber,
because additional leakage occurs at this piston/bushing-
contact. In addition to that, friction forces will occur in this
contact as well. Even if there is no relative motion between
the surfaces in this contact, hydrodynamic friction forces
due to the leakage will occur at the bushing and will be
measured by the force sensors. In order to be able to install a
dynamic pressure sensor and the compensation piston, dead
volume is added to the piston chamber of the measured
piston unit. Like the additional leakage due to the
compensation this will slow down the pressure build-up as
well.
For the reasons explained above, two separated common
rails are used in the rig. Thus, the pressure level in the
measured piston/bushing unit is completely decoupled from
the pressure level in the other two piston units. The pressure
levels in the two rails are adjusted by manually adjustable
pressure relief valves. Slightly different pressure levels as
well as different dynamic characteristics will occur in the
two rails. Furthermore, in a standard pump the housing is
pressurised (roughly 3 – 6 bar) and flushed by the flow of
the feeding pump. At this point this is not the case in the rig.
In order to avoid a force shunt between the pump housing
and the force measurement platform, no sealing is installed
between the housing and the bushing. As a consequence it is
not possible to pressurise the housing of the rig. The
flushing of the housing in the rig is only achieved by the
leakage of the three piston units and not by the total flow of
the supply pump. A further difference between pump and
test rig is that the fuel in the rig is pressurised several times.
In a common rail system the pressurised fuel is burned after
compression. Only a small amount is pressurised several
times. In the rig an aging of the diesel can occur during the
measurement, because it is pressurised and throttled several
times.
Some of those differences will be eliminated in future
measurements, see Chapter 5 of this paper.
2.3 Measurement Results
In a first step, measurement with standard diesel were
conducted to prove the functioning of the rig and to detect
weaknesses. Measurement results at a selected point of
operation (rail pressure: 1800 bar; revolution: 200 1/min)
are shown in fig. 6.
Drive motor
Fly wheel
Angle sensor
Force sensor
Test box
Measuring platform
Compensation piston
Measured piston
Drive shaft
b) Hydraulic diagramm
Feeding pump
Common rail
a) Test rig layout
439
Figure 6: Measurement results
The revolution starts at the outer dead center of the piston
with a rotation angle of 0°. From 0° to 180° the piston is
moving downwards (suction stroke) and from 180° to 360°
upwards (compression stroke). Forces during the suction
stroke are on a low level due to the low level of the piston
pressure of just a few bars. Just at the very beginning of the
suction stroke there is still a higher piston pressure level and
hence a higher level of forces. This higher level of piston
pressure is due to the compressibility of the fuel and the
elasticity of the components. At roughly 80° the
decompression is completed and the piston pressure stays on
the pressure level of the feeding pump. As soon as the
compression stroke is entered, the pressure in the piston
chamber raises. Due to a great amount of leakage in the
piston/bushing-contact of the measured piston unit and the
compensating piston as well as due to the compressibility of
the fuel and the elasticity of the solid bodies, the raise of the
pressure takes some time. At roughly 270° the piston
pressure reaches the pressure level of the rail. From then on,
fuel is delivered to the rail. A few degrees before the suction
stroke is entered the pressure level in the piston chamber
decreases. At this point the piston movement is not fast
enough to compensate the leakage losses. The transversal
forces on the piston Fx are submitted to a change in direction
at 270°, because at that point the relative motion in the
polygon/slipper-contact changes. This is also the case at 90°,
but at that point the change of direction is not visible in the
plots due to the low level of the force.
As exemplified before, the transversal load on the piston is
not just the friction force in the polygon/slipper-contact. The
transversal load of the cylinder Fx is equal to that friction
force Fµ only if the surface of the polygon ring is orthogonal
to the piston axis, see eq. 1. To detect the influence a tilting
of the polygon may have on the transversal load,
measurements with different displacements of the axis of the
measured piston unit to the drive shaft axis were conducted.
The test rig allows the variation of the displacement of the
measured piston unit from -2,5 mm up to +2,5 mm. The
results of these measurements are shown in fig. 7 (rail
pressure: 1800 bar; revolution: 200 rpm/min).
Figure 7: Measurement results for Fx with different
displacements
As it can be concluded from the results the displacement has
a huge influence on the transversal load on the piston. The
displacement of -2,5 mm leads to the highest transversal
load on the piston. The transversal load is reduced with
every step the displacement takes towards 2,5 mm. It can be
assumed that the friction force Fxμ in the polygon/slipper-
contact is independent of the displacement and has
approximately the same characteristic in all five
measurements due to comparable tribological operating
conditions of this contact. Hence, the variation in transversal
load Fx on the piston is caused by a different tilting
characteristic of the polygon ring.
To draw conclusions from the measurement results
concerning the most benificial displacement d is not
possible due to several reasons. Firstly, in the rig the
displacement of only one piston unit is changed. The
position of the other two piston units cannot be changed.
Secondly, up to now only one operating point is measured,
which is not a typical operating point of this kind of pump.
It can be expected that the most beneficial displacement is a
function of the operating conditions (revolution, pressure,
temperature) as well as of the tribological properties of the
fuel (lubricity and viscosity characteristic).
3 Simulative Approach
In the simulative approach, elastohydrodynamic models of
the fuel-lubricated contacts were set up. In the following, a
short introduction to the simulation tool will be provided.
For more detailed information regarding the simulation tool
the reader is referred to Knoll et al. [11, 12].
Solid bodies are incorporated in the simulation by FEM-
models. The local deformation and global rigid motion is
determined by the integration of a special formulation of
Newton’s equation of motion, which combines large rigid
body motions and small deformations of the elastic bodies,
see eq. (2). The properties of the elasic bodies are
incorporated in this equitation by the mass (M), damping
(D) and stiffness (K) matrices, which are obtained from
FEM-models. Centrifugal, gyroscopic and coriolis forces
arising on the right hand side of eq. 2 besides external
No
rma
lise
d f
orc
e [
-]
Drive shaft angle [°] Drive shaft angle [°]
No
rma
lise
d f
orc
e [
-]
d = 1,5 mm
d = 0 mm
d = 2,5 mm
d = -1,5 mm
d = -2,5 mm
rail pressure
Fx
Fz
piston pressure
440
forces. The total acceleration vector ( ̈ ̈) is separated
into rigid body ( ̈) and elastic accelerations ( ̈).
t+t+t+t=+++gycoceext
ffffuKuDuqM (2)
Prior to the elastohydrodynamic simulation, a reduction
scheme is applied in order to achieve acceptable
computation time by limiting the number of degrees of
freedom (DOFs) of conventional finite element models.
With the help of the reduction step, the modeling
capabilities of the structure are reduced to reasonable
deformation modes. It is important to choose relevant DOFs
for the reduction step, because all solutions in the reduced
system are weighted by superposition of these modes. In this
reduction procedure, which is called mixed Guyan/modal
reduction scheme, two different kinds of DOFs have to be
chosen. The first group, the so-called static Ritz vectors
model local deformations in stiff regions. These DOFs are
used to cover the local deformations of for example bearing
surfaces or surfaces were a load is applied. The second kind
of DOFs are the so-called modal Ritz vectors. These DOFs
represent the eigenvectors of the structure, which are
obtained from a modal analysis. With the help of these
DOFs global deformations can be represented by the
reduced structures. The static and modal Ritz vectors
represent the reduced DOFs and called static and modal
DOFs, respectively. The reduction step is done once for
each structure before the elastohydrodynamic simulation.
Besides standard coupling of different solid bodies by
means of springs and dampers the solid bodies can be
coupled via nonlinear hydrodynamic reaction forces which
represent lubricating films. Those hydrodynamic forces are
calculated on a separate 2d-mesh by solving Reynolds
equation for thin lubricating films, see eq. 3.
Microhydrodynamic effects are incorporated via flow
factors according to Patir and Cheng [13], which are gained
from measurements of real surface segments.
3;
12
3
i=
x
ph
xj
p
ij
i
t
h
x
vv
x
hvv
j
s
ijVii
i
ii
22
1212
(3)
Cavitation is considered by Reynolds boundary condition.
The different fuels are characterised by their viscosity
characteristics. Since high pressures and temperatures can
occur in injection systems, the temperature and pressure
dependency of the viscosity plays a major role. In order to
determine the fuel viscosity characteristic, a viscometer for
elevated pressure and temperature has been set up at IFAS
[14]. Based on these viscosity measurements, models were
parameterised and included in the simulation, see eq. 4.
11
0
0
0
z
p
p
z
p
e
(4)
As soon as the hydrodynamic forces cannot bear the entire
external forces on the lubrication film, solid body contact
occurs. The contact pressure is determined with the help of
the contact pressure curve. This curve is calculated based on
measurements of real surface segments. If a critical gap
height, which depends on the surface roughness of the parts
sliding against each other, is reached during the dynamic
analysis, solid body contact occurs. Friction forces are
calculated according to eq. 5.
dA
z
udApF
cccfriction
(5)
Up to now an energy equitation is not included in the
simulation tool and hence local temperatures cannot be
calculated by the simulation tool.
4 Simulation Models
4.1 First Simulation Models
In a first step simple simulation models for the
polygon/slipper-contact as well as for the piston bushing
contact were set up. In order to reduce simulation time,
those two lubricating films were simulated in separate
models. The simulated friction force in sliding direction
(polygon/slipper simulation) is transferred to the piston in
the piston/bushing simulation as transversal load. A more
detailed description of the models can be taken from [15].
The viscosity characteristic of the fuels is incorporated
according to eq. 4. The parameters are set according to
measurement results from a high pressure viscometer, which
was set up at IFAS. The results of those measurements for
several fuels at T = 40°C are displayed in fig. 8. The
intensive pressure dependency of some fuels becomes
obvious.
Figure 8: Pressure dependency of the viscosity at 40°C [16]
Fig. 9 shows the temperature dependency of some TMFB
candidates at atmospheric pressure. In Common-Rail-
Systems temperatures up to 120 °C and pressures up to
2000 bar have to be expected [17]. Hence, the temperature
as well as the pressure dependency cannot be neglected in
simulations.
441
Figure 9: Temperature dependency of the viscosity at
atmospheric pressure [16]
For the following simulations the promising fuel candidates
dibutylether (DBE), 2-Methyltetrahydrofuran (2-MTHF)
and butyl levulinate (BL) were chosen.
In fig. 10 simulation results for the bearing forces of the
contact are pictured. At closer inspection of the results for
the polygon/slipper-contact (left side of fig. 10) a huge
influence of squeeze-effects can be identified, which
reduces or even avoids solid body contact at the beginning
of the compression stroke at 180°. Those squeeze-effects are
viscosity-dependent and hence less distinctive for the fuel
candidates like DBE, 2-MTHF and BL with a low viscosity.
As a consequence, more solid body contact occurs if this
contact is lubricated with those fuel candidates This leads to
higher friction forces in the polygon/slipper-contact and
consequently to a higher transversal load on the piston in the
piston/bushing simulation. There, because of this higher
load and due to the lower viscosity, more solid body contact
occurs in this contact as well. All in all these results indicate
that this kind of pump design is sensitive to fuel viscosity.
Figure 10: Test rig, layout (a) and hydraulic diagram (b)
The comparability of those models to a real pump is limited.
For example the tilting of the polygon ring is not covered by
the models and hence the transversal load on the piston is
just the friction force Fxµ of the polygon/slipper-contact.
Furthermore, an almost ideal shape of the pressure in the
piston chamber was assumed. From 5° to 175° a constant
suction pressure level of 3 bar was assumed and from 185°
to 355° a constant injection pressure level. From 355° to 5°
and from 175° to 185° the commutations in-between the
pressure levels were assumed. As measurements at the test
rig have shown, the pressure in the chamber raises slowly
due to leakage, compressibility and elasticity.
4.2 Improved Models
In a next step those models were extended to achieve a
better comparability of the measurement and the simulation.
In the following these models – all in all three of them - are
presented. In a first simulation the tilting φ of the polygon is
detected. This tilting φ is an input for the second simulation.
In this simulation the contact between polygon and slipper is
modelled more accurately. The output of that simulation is
the transversal load Fx on the piston. The piston bushing
contact is calculated in the last simulation. The reason for
three separate models instead of one model for the whole
pump is once again the required computation time.
4.2.1 Tilting of the Polygon Ring
As measurements indicated, the tilting φ of the polygon ring
has a huge influence on the transversal load Fx on the piston,
see fig. 3. To consider this in the simulation, an additional
elastohydrodynamic simulation tool was set up, see fig. 11.
The piston pressure input, which is displayed in fig. 11 as
well, was determined a priori in a separate hydraulic
simulation with the simulation tool DSHplus. This model
consists of eight rigid or non-rigid solid bodies:
piston (three times); rigid (0 DOFs)
slipper (three times); non-rigid (50 DOFs)
polygon ring (one time); non-rigid (100 DOFs)
eccentric shoulder (one time); non-rigid (50 DOFs)
Figure 11: Simulation model for the tilting of the polygon
The eccentric shoulder is coupled with the polygon via a
rotational journal bearing (140 nodes) and the three slippers
piston
slipper
ω
p1(shaft angle)
p2(shaft angle)
crank shaft angle [deg]
p3(shaft angle)
polygon
eccentric
shoulder
pis
ton p
ress
ure
[bar
]
442
are coupled to the polygon via axial journal bearings (71
nodes). All bearings are lubricated with fuel. The way the
piston is coupled to the slippers has a high influence on the
tilting of the polygon. In the pump, the piston is held down
to the slipper by a small metal clip, see fig. 12. This clip
does not block a tilting up to a tilting angle of 4° in both
directions. As soon as piston and slipper axis are not
concentric, not the whole bottom surface transfers the load
from the piston to the slipper. On one side of the contact a
gap arises and on the other side the load is transferred via
solid body contact pressure of the contacting surfaces. In the
simulation this characteristic could be modelled with the
help of a lubricating film. But since the computation effort
to solve the Reynolds equitation on this film and to
determine the contact pressures on the bearing surfaces is
huge, this option is not implemented in the simulation
model. Instead another solution, which reduces computation
time dramatically, is chosen. Each piston is coupled with its
slipper via three compression springs, see fig. 12. With this
kind of coupling the basic characteristic of the contact
between piston and slipper in the pump can be modelled,
assuming an adequate parameterisation of those three
springs.
Figure 12: Coupling of piston and slipper
4.2.2 Polygon/Slipper-Contact
The second simulation is a more precise simulation of the
polygon/slipper-contact, see fig. 13. In this simulation only
one lubricating fuel film is covered and there are only three
solid bodies:
piston; non-rigid (0 DOFs)
slipper; non-rigid (250 DOFs)
1/3 polygon; non-rigid (300 DOFs)
Figure 13: Simulation model for the polygon/slipper-contact
The polygon is tilted as a function of the shaft angle
according to the results of the first simulation. In order to
get more accurate results the number of DOFs of the slipper
and polygon is increased in comparison to the first
simulation. Furthermore, the 2d-mesh representing the
lubricating film between slipper and polygon is defined
more precisely (1871 nodes). The piston is modeled as a
rigid body. The coupling between piston and slipper is
implemented by three compression springs again. This
simulation delivers as a result the transversal load Fx on the
piston as a function of the shaft angle.
4.2.3 Piston/Bushing-Contact
The third and last model is a more accurate model of the
piston/bushing-contact, see fig. 14.
Figure 14: Simulation model for the piston/bushing-contact
The solid bodies, the piston and the bushing, are modeled as
non-rigid bodies with 100 DOFs and 300 DOFs
respectively. The lubricating film along the piston/bushing-
contact is represented by a 2d-mesh with 1936 nodes. Along
the gap in axial direction the pressure level is reduced by
throttling effects. At the top end of the piston the pressure is
on a high level during the compression stroke and at the
lower end the pressure level is equal to the pressure level in
the pump housing. The fuel is throttled from the piston
chamber pressure level to the pressure level in the housing,
as it can be seen in the fuel pressure distribution in fig. 13.
In real pumps this energy dissipation leads to a heating of
the fuel along the gap. Since the energy equation is not
implemented in the model, thermal effects are included in a
simplified manner. As measurements in literature show [18],
the temperature distribution along the bushing is
approximately linear. This knowledge is used to define a
temperature-dependent reference viscosity η0 along the z-
direction of the lubricating gap.
4.3 Simulation Results
In the following some results of the improved models are
presented. The simulated operating point is the same like in
fig. 10 (rail pressure: 1350 bar; revolution: 2500 1/min,
temperature: 50 – 100°C).
bushing
piston
slipper
φ
φ
0L
EAc i
i
0ic
p1(shaft angle)
x0
compression springs
clamp
p1(shaft angle)
p1(shaft angle)
piston (rigid)
slipper (non rigid)
pressure distribution
1/3 polygon
(non rigid) φ (shaft angle)
piston (non rigid)
fuel pressure
contact pressure
bushing (non rigid)
443
Figure 15: Results regarding the tilting of the polygon
In fig. 15 the simulated tilting of the polygon is plotted. A
periodic characteristic is visible. Every 120° a peak up to
1.8° occurs due to the commutation. The dashed line
represents the simulation results for the tilting of the
polygon in the test rig. This tilting differs from the tilting in
a standard pump due to the deviating pressure build-up in
the measured piston unit (piston 1) in comparison to the
other two piston units in that test rig. As explained before,
the pressure build-up in the measured piston unit is slowed
down by leakage at the compensation piston and by an
increased dead volume.
Figure 16: Results regarding friction forces of the
polygon/slipper-contact and the transversal load on the
piston
Figure 16 shows the friction forces in the polygon/slipper-
contact and the transversal load Fx on the piston. Besides the
total friction force Fµ its share resulting from solid body
friction and its share due to hydrodynamic friction are
plotted. The hydrodynamic share is neglectable so that
almost all the friction in this contact is due to solid body
friction. Because a tilting of the polygon occurs, the
transversal load deviates from the total friction force. Only
when the tilting angle is zero the transversal force Fx is
identical to the friction force Fµ, e.g. at 325°.
Comparing the simulation results for the transversal load on
the piston of the first simulation models plotteted in fig. 10
(upper left side) to the results of the improved models it is
visible that the transversal load simulated with the improved
models is oscillating due to tilting of the ring. This
characteristic is not visible in the results of the first models
in fig. 6. There the transversal load is steadily rising during
the compression stroke. In the measurement results plotted
in fig. 6 and 7 an oscillating characteristic similar to the
results of the improved models is visible, too. Neverthless, a
comparison of measurement and simulation is disputable at
this point because of different operating points in the
simulation and the measurement.
Figure 17: Results regarding contact forces of the polygon
slipper-contact
In fig. 17 the contact forces in the polygon/slipper-contact
are presented. Again distinctive squeeze-effects at the
beginning of the compression stroke are visible. Solid body
contact is avoided or reduced by these effects at the
beginning and hence the friction force in x-direction starts
on a low level. Later on, this effect decreases and
consequently more and more of the load is carried by solid
body contact.
Figure 18: Results regarding friction forces of the
slipper/polygon-contact
Figure 18 presents the friction forces in the piston/bushing-
contact. Again, the total friction force is divided into its
hydrodynamic friction share and its contact friction share. In
contrast to the polygon/slipper-contact, the hydrodynamic
444
friction share is not negligible. Because of the huge pressure
difference during the compression stroke of 1350 bar an
intensive poiseuille flow leads to a hydrodynamic friction
force of roughly 20 N. Because of the transversal load on
the piston solid body contact occurs and hence a solid body
friction force.
5 Conclusion and Outlook
In this paper an experimental and simulative approach for
investigating the impact of new biofuels on the tribological
contacts in common rail pumps was presented. Potential for
further improvements on the experimental side and first
results were discussed. These results are indicating a huge
influence of the tilting φ of the polygon on the transversal
load Fx on the piston. On the simulative side first simulation
models and results for different fuels were presented. Those
first models do not capture the tilting of the ring. In order to
achieve a better compatibility with the measurements, the
simulation models were improved and extended. The results
for diesel show a better compatibility to the measurements,
but a validation of the simulation by the measurement is not
possible at this time, because there are several drawbacks
mainly on the experimental side. To further increase
comparability, improvements of the test rig will be done.
This includes improvements of the pressure control in the
rail, a better capturing of local temperatures and leakage
measurements at the piston or at the compensation piston.
After those modifications, testing of more typical operating
points at higher speeds of more than 1000 rev/min will be
possible as well as testing of different fuels.
6 Acknowledgement
This work was supported by the Deutsche Forschungs-
gemeinschaft (German Research Foundation) within the
cluster of excellence 236 “Tailor-made Fuels from Biomass”
[EXC 236].
Nomenclature
Designation Denotation Unit
A Area [m2]
fce Centrifugal force [N]
x Coordinate [m]
fco Coriolis force [N]
D Damping matrix
ρ Density [kg/m3]
d Displacement [m]
e Eccentricity [m]
E E-module [N/m2]
fext External force [N]
Φ Flow factor [-]
Fi Force [N]
µ Friction coefficient [-]
h Gap height [m]
fgy Gyroscopic force [N]
L Length [m]
M Mass matrix
p Pressure [bar]
c Spring stiffness [N/m]
K Stiffness matrix
T Temperature [°C]
φ Tilting angle [°]
t Time [s]
v Velocity [m/s]
η Viscosity [(N s)/m2]
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